An afterbody for a rotor blade of a rotorcraft is unitarily formed of a single material of construction. The afterbody includes an upper surface disposed from a lower surface, a concave leading edge connected to the upper surface and the lower surface, and a trailing edge formed at an intersection of the upper surface with the lower surface.
Rotor blade afterbody
2020-07-14
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
Lobed nozzle afterbody research
Tema Archive | 1987
|Lobed nozzle afterbody research
AIAA | 1987